NSN 9540-01-353-5553

Part Details | STRUCTURAL ANGLE

9540-01-353-5553 A structural shape fabricated from a ferrous or nonferrous material and resembling the letter L in cross-sectional form. The edges may have a bulb, be rounded, and the inside corner may have a fillet.

Alternate Parts: LS 0430294, LS 043-0294, QQA2003, QQ-A-200/3, AMSQQA2003, AMS-QQ-A-200/3, 60702024T3511, 60-70/2024-T3511, 9540-01-353-5553, 01-353-5553, 9540013535553, 013535553

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
95FEB 12, 199201-353-555337017 ( ANGLE, STRUCTURAL )
REFERENCE DRAWINGS & PICTURES

ANGLE

RIGHT QUARTER RADIUS

UPPER RADIUS

RIGHT QUARTER RADIUS

UPPER RADIUS

Cross Reference | NSN 9540-01-353-5553
Part Number Cage Code Manufacturer
LS 043-029443999BOEING COMPANY, THEDBA BOEING
QQ-A-200/381348FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES
AMS-QQ-A-200/381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
60-70/2024-T351129321TRANSTAR METALS CORP
Technical Data | NSN 9540-01-353-5553
Characteristic Specifications
MATERIAL ALUMINUM ALLOY 2024
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-200 TO 3 FED SPEC 1ST MATERIAL RESPONSE
FABRICATION METHOD EXTRUDED
HEAT TREATMENT T-3511 SOLUTION HEAT TREATED
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
BASIC SHAPE STYLE ANGLE
OVERALL HEIGHT1.000 INCHES NOMINAL
OVERALL WIDTH1.000 INCHES NOMINAL
LEFT SIDE FLANGE THICKNESS0.062 INCHES NOMINAL
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.062 INCHES NOMINAL
BASE FLANGE THICKNESS0.062 INCHES NOMINAL
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
FIRST TIP STYLE RIGHT QUARTER RADIUS
FIRST TIP RADIUS0.031 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIP NOT IDENTICAL
SECOND TIP STYLE UPPER RADIUS
SECOND TIP RADIUS0.031 INCHES NOMINAL
WEIGHT PER UNIT MEASURE0.145 POUNDS PER LINEAR FOOT
NONDEFINITIVE SPEC/STD DATAT3511 TEMPER